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公开(公告)号：US20210403150A1
公开(公告)日：2021-12-30
申请号：US17287744
申请日：2020-03-31
申请人： VINATI S.R.L.
摘要： An aircraft (100) with a rotary wing (40) is equipped with a propulsion system (10). The aircraft (100) includes a rotating mast (50) that rotates the rotor wing (40). The propulsion system (10) includes a pole (20) mechanically connected to the rotating mast (50) of the aircraft (100), where at least one end of the pole (20) is equipped with a motor (30) configured to rotate the pole (20) around the axis of the rotating mast (50) in such a way that the rotation of the pole (20) can be used to rotate the rotating wing (40). At each end of the pole (20) is placed a motor group (30), where each motor group (30) includes a pair of counter-rotating propellers (32,32), said pair of counter-rotating propellers (32,32′) being arranged in such a way as to generate a rotational torque to rotate the pole (20).
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公开(公告)号：US11858619B2
公开(公告)日：2024-01-02
申请号：US17287744
申请日：2020-03-31
申请人： VINATI S.R.L.
CPC分类号： B64C27/18 , B64C27/001 , B64D27/24 , B64D35/06 , B64C2220/00
摘要： An aircraft (100) with a rotary wing (40) is equipped with a propulsion system (10). The aircraft (100) includes a rotating mast (50) that rotates the rotor wing (40). The propulsion system (10) includes a pole (20) mechanically connected to the rotating mast (50) of the aircraft (100), where at least one end of the pole (20) is equipped with a motor (30) configured to rotate the pole (20) around the axis of the rotating mast (50) in such a way that the rotation of the pole (20) can be used to rotate the rotating wing (40). At each end of the pole (20) is placed a motor group (30), where each motor group (30) includes a pair of counter-rotating propellers (32,32), said pair of counter-rotating propellers (32,32′) being arranged in such a way as to generate a rotational torque to rotate the pole (20).
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公开(公告)号：US11820497B2
公开(公告)日：2023-11-21
申请号：US16483928
申请日：2018-08-03
申请人： VINATI S.R.L.
摘要： A rotor wing aircraft provided with a propulsion apparatus is disclosed. The aircraft has a rotating mast configured to rotate said rotor wing and the apparatus includes a pole mechanically connectable to the rotating mast of the aircraft. At one of the ends of the pole there is placed an electric turbine, powered by a battery, and configured to rotate the pole around an axis of the rotating mast in such a way that the rotation of the pole can be used to rotate the rotor wing. Preferably the pole is made of carbon fiber.
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公开(公告)号：US11112766B2
公开(公告)日：2021-09-07
申请号：US15777926
申请日：2016-11-18
申请人： VINATI S.R.L.
发明人： Felice Vinati , Samuele Vinati , Matteo Vinati , Mariachiara Vinati , Giacomo Vinati , Fabio Previdi , Alberto Cologni , Michele Ermidoro , Luca Bortolotti
IPC分类号： G05B19/402 , B66C13/40 , G01C21/08 , G05B19/409 , G01C21/16
摘要： A method of estimating an attitude of a control device for controlling operating machines, where the control device has a plurality of pushbuttons for controlling the movement of an operating machine along respective directions, the method having the following steps: —preliminary estimating the attitude of the control device using data from an accelerometer and a magnetometer onboard of the control device; —updating of the preliminary estimate of the attitude of the control device using data from a gyroscope onboard of the control device.
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5.发明授权公开(公告)号：US09919901B2
公开(公告)日：2018-03-20
申请号：US15038729
申请日：2014-11-06
申请人： VINATI S.R.L.
发明人： Sergio M. Savaresi , Felice Vinati , Samuele Vinati , Matteo Vinati , Mariachiara Vinati , Giacomo Vinati
CPC分类号： B66C13/063 , B66C13/30 , B66C17/00
摘要： A device for controlling a swinging of a load suspended from a motorized slidable element is described. The controlling device includes a control unit and an inertial platform. The control unit is provided with means to measure and control the speed of the motorized slidable element and is able to process the values representative of the inclination angle of the cable with respect to the vertical to calculate and to impart control actions in order to dynamically control the speed of the motorized slidable element as a function of a desired inclination angle of the cable with respect to the vertical.
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